Other Limitations and Knowledge

Question 1

Is the aircraft certified for ditching when appropriate safety equipment is installed?

Answer 1

Yes

Question 2

Maneuvering Load Limit Flaps Up

Answer 2

+2.6 to -1.0

Question 3

Maneuvering Load Limit Flaps Extended

Answer 3

+2.0 to 0.0

Question 4

Maximum Pressure Altitude for Flight

Answer 4

FL450

Question 5

When Type II, III, IV anti-icing funds have been applied the wing anti-ice system must only be selected on…?

Answer 5

just prior to thrust application for takeoff.

Question 6

In accordance with FCOM, Supplement 1, -Cold Weather Operations, takeoff IS permitted with frost adhering to the:

(2)

Answer 6

a) underside of the wing that is caused by cod soaked fuel.

b) Upper surface of the fuselage

Question 7

Selecting the AIR SOURCE switch to TRIM AIR ONLY is prohibited when?

Answer 7

The aircraft is on the ground

Question 8

The ________ must be operating when the aircraft electrical power is ON for more than 30 minutes and the OAT is >40C (104F)

Answer 8

PACK

Question 9

Crew and Passenger oxygen masks are only approved up to what cabin altitude?

Answer 9

40,000 feet

Question 10

Prolonged operation of passenger oxygen masks above what altitude is not recommended?

Answer 10

25,000 feet

Question 11

Maximum differential pressure on the ground is?

Answer 11

0.1 psi

Question 12

Maximum differential pressure during landing must not exceed?

Answer 12

1.0 psi

Question 13

Maximum positive differential pressure is?

Answer 13

9.4 psi

Question 14

Maximum negative differential pressure is?

Answer 14

-0.5 psi

Question 15

Autopilot minimum engaged height on Climbs, Enroute flight, and Descent is?

Answer 15

700’ AGL

Question 16

Autopilot minimum use height on a Precision Approach with a glide slope angle of 3.5 degrees or less is?

Answer 16

80’ AGL

Question 17

Autopilot minimum use height on a Precision Approach with a glide slope angle between 3.5 to 4.5 degrees is?

Answer 17

160’ AGL

Question 18

Autopilot minimum use height on a Visual or Non-Precision approach is?

Answer 18

200’ AGL

Question 19

Maximum altitude with Yaw Damper OFF is?

Answer 19

31,000’

Question 20

Required Equipment for RVSM?

Answer 20

1. Operational Autopilot
2. Operational Altitude Alerting System
3. One Operational Altitude Reporting Transponder
4. Two Operational Air Data Computers

Question 21

To use the FMS as a Navigation Source it must be receiving navigation information from the following:

Answer 21

a. Two GNSS -or-
b. Two DMEs -or-
c. One VOR/DME -or-
d. One IRS

Question 22

Use of the FMS Secondary flight plan function is?

Answer 22

Prohibited

Question 23

Use of FMS navigation South of 60 degrees S is?

Answer 23

Prohibited

Question 24

Use of FMS navigation North of 73 degrees N is?

Answer 24

Prohibited

Question 25

RNP APCH CDI Scale is?

Answer 25

0.3 nm

Question 26

Basic RNP-1 CDI Scale is?

Answer 26

1.0 nm

Question 27

RNP-2 CDI Scale is?

Answer 27

2.0 nm

Question 28

RNP-4 CDI Scale is?

Answer 28

4.0 nm

Question 29

RNP-10 CDI Scale is?

Answer 29

4.0 nm

Question 30

What must be annunciated on the PFD in order to use an FMS approach?

Answer 30

RNP APPR or LPV APPR

Question 31

What type of approach is prohibited with the Standby Instrument?

Answer 31

Localizer Backcourse

Question 32

Do not extend the Flaps above?

Answer 32

FL180

Question 33

Do not extend Flight Spoilers except during an ___________?

Answer 33

Emergency Condition

Question 34

Flight Spoilers must not be extended in flight at airspeeds below?

Answer 34

Approach Speed +8 KIAS

Question 35

Flight Spoilers must not be extended in flight below _____AGL.

Answer 35

500'

Question 36

Do not extend the landing gear above?

Answer 36

FL180

Question 37

Max continuous Amps with 2 or 3 generators?

Answer 37

400 amps

Question 38

Max continuous Amps 1 generator on the ground?

Answer 38

400 amps

Question 39

Max continuous Amps 1 generator in flight?

Answer 39

500 amps

Question 40

Max continuous Amps Transient (5 minutes)

Answer 40

600 amps

Question 41

Usable Fuel Load with Pressure fueling?

Answer 41

14,150

Question 42

Usable Fuel Load with Gravity fueling?

Answer 42

13,000

Question 43

Approved Fuels?

Answer 43

Jet A, JETA1, JET B, JP-4, JP-5, JP-8. JET B and JP-4 maximum altitude 16,000'

Question 44

CL350 Engine Type and Thrust

Answer 44

HTF7350 | 7,323 lbs of thrust

Question 45

The engines must be motored for _____ seconds after an aborted start.

Answer 45

30 seconds

Question 46

How many engine start cycles may be attempted?

Answer 46

3 consecutive start cycles followed by a 15 minute cooling period.

Question 47

Reverse Thrust is limited to Idle Reverse below _____KIAS.

Answer 47

40 KIAS

Question 48

APU Maximum altitude to be operated?

Answer 48

37,000'

Question 49

APU Maximum Altitude to be used as a generator?

Answer 49

30,000'

Question 50

APU Maximum altitude to use Bleed Air for Engine Start?

Answer 50

20,000'

Question 51

APU Maximum altitude to use Bleed Air for ECS?

Answer 51

20,000'

Question 52

Do not use APU to start the left engine on the ground above?

Answer 52

9,000'

Question 53

Can the APU be operated during fluid deicing/anti-icing?

Answer 53

NO

Question 54

The APU may be started up to an altitude of? | Ground/Flight

Answer 54

30,000' Flight | 14,000' Ground

Question 55

What numbers/time do you watch for when starting APU? | hung start

Answer 55

RPM 30% within 30 seconds.

Question 56

APU starting attempt limitations?

Answer 56

1-1 minute 2-1 minute 3-20 minutes 4 and 5 may then be attempted followed by a cooling period of 40 minutes.

Question 57

Flexjet APU Airstart limitation?

Answer 57

250 KIAS, 10,000; maximum, 1 attempt.

Question 58

APU maximum RPM?

Answer 58

108%

Question 59

APU Start EGT Limit?

Answer 59

973C

Question 60

APU Normal Operations EGT?

Answer 60

718C.

Question 61

CAS messages are inhibited on takeoff when?

Answer 61

Starts when you accelerate through 80 knots. Ends when you reach 400’ or 60 seconds.

Question 62

CAS messages are inhibited for landing when?

Answer 62

Starts when you descend through 400’. Ends when you decelerate through 40 knots or 60 seconds.